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Connecting device of ground testing equipment of aircraft

A technology of ground testing equipment and connecting devices, which is applied in transmission monitoring, digital transmission systems, electrical components, etc., and can solve problems such as being unable to connect to the Internet

Active Publication Date: 2015-02-18
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to overcome the defect that the existing Chinese and Russian satellite ground test equipment cannot be networked, thereby providing a connecting device for aircraft ground test equipment

Method used

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  • Connecting device of ground testing equipment of aircraft
  • Connecting device of ground testing equipment of aircraft
  • Connecting device of ground testing equipment of aircraft

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Experimental program
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Embodiment Construction

[0016] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0017] In one embodiment, Party A and Party B each have ground test equipment for aircraft electrical testing. In order to achieve the purpose of joint electrical testing, a connecting device is added between the ground testing equipment of both parties. One end of the ground test equipment connection device is connected to the network environment of Party B's ground test equipment, and the other end is connected to the network environment of Party A's ground test equipment.

[0018] According to the requirements of the joint electrical test, the ground test equipment of both parties shall perform the following operations through the connection device of the ground test equipment:

[0019] Establish a network connection, including:

[0020] (1) Log in to Party A's test server;

[0021] (2) Log in to the ground control computer of Party B.

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PUM

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Abstract

The invention discloses a connecting device of ground testing equipment of an aircraft. The connecting device comprises a first communication module, a first party protocol data packet splitting module, a second party protocol data packet encapsulating module, a second party protocol data packet splitting module, a first party protocol data packet encapsulating module and a second communication module, wherein the first communication module is connected to the first party protocol data packet splitting module; the first party protocol data packet splitting module is connected with the second party protocol data packet encapsulating module; the second party protocol data packet encapsulating module is further connected to the second communication module; the second communication module is connected to second party combined electrical ground testing equipment and also connected to the second party protocol data packet splitting module; the second party protocol data packet splitting module is further connected to the first party protocol data packet encapsulating module; and the first party protocol data packet encapsulating module is finally connected to the first communication module.

Description

technical field [0001] The invention relates to the field of satellite ground testing, in particular to a connection device for aircraft ground testing equipment. Background technique [0002] The joint Mars exploration is that Party A’s small aircraft is carried on Party B’s aircraft. During the fire cruising section, Party B’s aircraft will receive the remote control data sent by the ground measurement and control system and forward it to Party A’s small aircraft, and at the same time forward the telemetry data of Party A’s small aircraft to the ground. Measurement and control system; after the aircraft complex arrives at Mars, the aircraft will be separated, and Party A's small aircraft will fly around Mars independently. [0003] Aircraft electrical measurement is an important work in the process of aircraft development. By implementing electrical testing on the aircraft, ensure that the functions and performance of the aircraft meet the requirements. Such as figure 1...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04L12/26H04L29/06H04B17/00
Inventor 刘利军朱新波陈昌亚张奎彬
Owner SHANGHAI SATELLITE ENG INST